NASA NTRS · 19700060332
Conical shock-wave turbulent boundary-layer interaction including suction effects
Abstract
Conical shock wave-turbulent boundary layer interaction data obtained for adiabatic wall conditions at supersonic free stream Mach numbers, including suction effects
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Childs, M. E., Seebaugh, W. R.. 1970-08-01. Conical shock-wave turbulent boundary-layer interaction including suction effects. https://ntrs.nasa.gov/citations/19700060332
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